Honeywell SPZ-8000 Pilot's Manual page 222

The pilot steps through the tests using the L AFCS button until 98 L
FLIGHT FAULT SUMMARY is displayed as shown in Figure 9--4.
When the RESET button is pushed, data is displayed for the first flight
guidance computer, as shown in Figure 9--5.
The alphanumeric codes should be recorded for use by Honeywell
personnel in troubleshooting the problems. When the RESET button is
pushed again, the fault data for the second flight guidance computer is
displayed.
A28--1146--055
REV 2
SPZ--8000 Digital Integrated Flight Control System
Final Flight Fault Test
Figure 9--4
Flight Fault Summary
Figure 9--5
Troubleshooting
9-9